US4011565A - Method of determining ionospheric reflection height - Google Patents

Method of determining ionospheric reflection height Download PDF

Info

Publication number
US4011565A
US4011565A US05/678,321 US67832176A US4011565A US 4011565 A US4011565 A US 4011565A US 67832176 A US67832176 A US 67832176A US 4011565 A US4011565 A US 4011565A
Authority
US
United States
Prior art keywords
height
reflection
hop
doppler
boundary
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US05/678,321
Inventor
Kurt Toman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
US Air Force
Original Assignee
US Air Force
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by US Air Force filed Critical US Air Force
Priority to US05/678,321 priority Critical patent/US4011565A/en
Application granted granted Critical
Publication of US4011565A publication Critical patent/US4011565A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S3/00Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/02Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves

Definitions

  • Phase path P defined with reference to the transit time T p , between a transmitter T and receiver R, of a surface of constant phase, may be expressed as ##EQU1## WHERE ⁇ IS THE REFRACTIVE INDEX, ⁇ THE ANGLE BETWEEN WAVE NORMAL AND RAY DIRECTION, AND DS IS AN ELEMENT OF THE RAY PATH ALONG WHICH THE INTEGRATION IS PERFORMED.
  • a method has been developed that permits determination of ionospheric reflection height from doppler measurements. For this method it is required that doppler signatures ⁇ f(t) of at least two transmissions, involving for example, one single-hop and one multi-hop, are simultaneously detectable.
  • the novel feature is that phase-path variations, caused by a moving reflection boundary, can be utilized to determine the reflection height by means of the rate-of-change of phase-path information of two transmissions involving a pair of available transmission paths being comprised of multi-hops or a single- and a multi-hop.
  • a method of determining ionospheric reflection height from doppler measurements made over an oblique radio transmission involving reflection of signals from a boundary makes use of multi-hop reflections.
  • the unknown motion of the reflection boundary is eliminated by taking the doppler-shift ratio for a pair of transmission hops.
  • the height of the reflection boundary is then computed from this ratio for the particular distance that separates transmitter from receiver.
  • the equations used follow from relatively simple geometrical considerations derived from physical boundaries.
  • FIG. 1 illustrates the total path length between the transmitter, reflection boundary, and receiver, with H being the reflection height, R e the earth radius, and ⁇ corresponds to the angular distance between the transmitter and receiver;
  • FIG. 2 illustrates the behavior of the ratio as a function of reflection height
  • FIG. 3 illustrates the frequency variations over a specified period of time.
  • the method of this invention permits determination of ionospheric reflection height from doppler measurements.
  • a radial motion, dH/dt of this mirror-like boundary imparts different rate-of-phase-path changes (dP/dt) to the 1-hop, 2-hop, n-hop transmissions causing doppler shifts
  • Equation (5) is solved parametrically for D.
  • Equations (5) and (6) yield the ratio for this limiting condition, as illustrated in FIG. 2 by the dots separating solid and dashed lines. In the limit of D ⁇ 0 (H ⁇ O) this limiting ratio equals 2.5. For increasing values of D the ratio decreases and approaches 2 for D ⁇ ⁇ R e while H min ⁇ .
  • FIG. 3 illustrates the frequency variations observed from 1600 to 2100 EST on Mar. 1, 1969.
  • ⁇ f o 0.62 Hz

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

A method for determining the ionospheric reflection height from doppler measurements made over an oblique radio transmission involving reflection of signals from a boundary. This method makes use of multi-hop reflections. The unknown motion of the reflection boundary is eliminated by taking the doppler-shift ratio for a pair of transmission hops. The height of the reflection boundary may be computed from this ratio for the particular distance that separates transmitter from receiver. The equations used follow from relatively simple geometrical considerations derived from spherical boundaries.

Description

STATEMENT OF GOVERNMENT INTEREST
The invention described herein may be manufactured and used by or for the Government for governmental purposes without the payment of any royalty thereon.
BACKGROUND OF THE INVENTION
Ionospheric doppler measurements made at the carrier frequency of an oblique radio transmission provide a very sensitive means of measuring ionospheric phase path variations, but preclude the determination of phase path, from which a reflection height could be inferred because of phase ambiguity. Phase path P defined with reference to the transit time Tp, between a transmitter T and receiver R, of a surface of constant phase, may be expressed as ##EQU1## WHERE μ IS THE REFRACTIVE INDEX, β THE ANGLE BETWEEN WAVE NORMAL AND RAY DIRECTION, AND DS IS AN ELEMENT OF THE RAY PATH ALONG WHICH THE INTEGRATION IS PERFORMED. In solving equation (1) it is necessary that the relevant properties of the medium are known such that radio-rays, originating from the transmitter, T, and reaching the receiver R via the medium, can be specified. In an experimental setup the reverse procedure is prevalent, when it is of interest to deduce a reflection height from propagation data without knowing the detailed specifications of the propagation medium.
A method has been developed that permits determination of ionospheric reflection height from doppler measurements. For this method it is required that doppler signatures δf(t) of at least two transmissions, involving for example, one single-hop and one multi-hop, are simultaneously detectable. The novel feature is that phase-path variations, caused by a moving reflection boundary, can be utilized to determine the reflection height by means of the rate-of-change of phase-path information of two transmissions involving a pair of available transmission paths being comprised of multi-hops or a single- and a multi-hop.
SUMMARY OF THE INVENTION
A method of determining ionospheric reflection height from doppler measurements made over an oblique radio transmission involving reflection of signals from a boundary. This method makes use of multi-hop reflections. The unknown motion of the reflection boundary is eliminated by taking the doppler-shift ratio for a pair of transmission hops. The height of the reflection boundary is then computed from this ratio for the particular distance that separates transmitter from receiver. The equations used follow from relatively simple geometrical considerations derived from physical boundaries.
DESCRIPTION OF THE DRAWINGS
FIG. 1 illustrates the total path length between the transmitter, reflection boundary, and receiver, with H being the reflection height, Re the earth radius, and α corresponds to the angular distance between the transmitter and receiver;
FIG. 2 illustrates the behavior of the ratio as a function of reflection height; and
FIG. 3 illustrates the frequency variations over a specified period of time.
The method of this invention, as illustrated in the apparatus of FIG. 1, permits determination of ionospheric reflection height from doppler measurements. For this method it is required that doppler signatures δf(t) of at least two transmissions, involving for example one single-hop and one multi-hop, are simultaneously detectable. It is assumed that all reflections occur at the same height, H, of a spherical boundary (Re +H), that is concentric to a spherical earth (Re = 6378 km). A radial motion, dH/dt of this mirror-like boundary imparts different rate-of-phase-path changes (dP/dt) to the 1-hop, 2-hop, n-hop transmissions causing doppler shifts
δf.sub.n = -(f/c)(dP/dt ).sub.n                      2.
where f represents the carrier frequency of the transmission, c the velocity of light in vacuum and n the number of hops. Since ##EQU2## it is possible to determine δfn, provided (dP/dH)n and (dH/dt) are known. While (dP/dH)n is easily derivable from the geometrical configuration of the transmissions, (dH/dt) is not known. The ratio (dP/dH)n can be expressed as ##EQU3## where P is the total path length between transmitter, reflection boundary, receiver, H is the reflection height, Re the earth radius; α corresponds to the angular distance (α = D/Re) between transmitter and receiver as illustrated in FIG. 1. The unknown rate-of-change of height with time (dH/dt) in equation (3) can be eliminated by using equation (4) and taking, for example, the ratio (dP/dt)2hop /dP/dt)1 hop. Accordingly, ##EQU4## Equation (5) is solved parametrically for D.
FIG. 2 illustrates the behavior of the ratio (dP/dH)n =2 /(dP/dH)n =1 as a function of reflection height H, for D = αRe =0, 100, 500 and 2000 km. Knowing the doppler ratio of the two- and one-hop transmissions, FIG. 2 can be used for inferring the reflection height. It is noted, however, that there exist two solutions of H, both physically meaningful. The height separation of these solutions varies with distance D. General knowledge about the reflection height, expected for a particular radio frequency and for a broad range of ionospheric conditions, permits selection of the plausible solution and rejection of the other. Comparing, for example, the general behavior of these curves with distance, it is seen that for short distances (D<<100 km) the effectiveness in height resolution is limited to the non-ionized portion of the atmosphere (H< 60 km). For D = 500 km, the height resolution of the ratio-method may be optimal for about 80 km < H <140 km, but continues to be acceptable up to H = 350 km. A ratio r = 2.6, for example, yields H1 = 5.5 km, H2 = 220 km.
For D = 0 (FIG. 2) the ratio r equals two for all values of H and the ratio method is clearly useless for finding any reflection height. Curiously, for a spherical earth and for all values of D, the limit of r is almost unity as H → 0 and equals unity for D = H = 0. The dashed portions of the curves of FIG. 2 indicate, however, that the rays describing P.sub.(1 hop) intersect the spherical earth before reaching a particular reflection height and are thus not meaningful in the context of satisfying a realizable reflection condition. The limiting condition is obtained when departing/arriving rays are tangent to the earth. This condition follows from ##EQU5## which relates the minimum height of reflection to angular distance between transmitter and receiver. Equations (5) and (6) yield the ratio for this limiting condition, as illustrated in FIG. 2 by the dots separating solid and dashed lines. In the limit of D→ 0 (H→O) this limiting ratio equals 2.5. For increasing values of D the ratio decreases and approaches 2 for D→ π Re while Hmin →∞.
The method described above was applied to doppler measurements made over an oblique 7.335 MHz transmission from Time Station CHU, Ottawa, Canada, to AFCRL, Bedford, Mass. (D = 480 km). FIG. 3 illustrates the frequency variations observed from 1600 to 2100 EST on Mar. 1, 1969. Of particular interest for this study is the time interval 1900 - 2000 EST. An undulation of the doppler signature commences at 1916 EST, starting with zero doppler as deduced from ionospheric E-region reflections observed at noon, reaching a negative doppler shift of δfo = 0.62 Hz, relative to zero, at 1928 EST and returning to zero at 1940 EST. For the same time interval, a second trace showing larger excursions in doppler shift is observed. Because of the similarity between these doppler signatures, it is assumed that the trace with the larger excursion represents the two-hop transmission, the other the one-hop transmission. Determining the ratio of these doppler shifts at 1930 EST using equations (3) and (5), one obtains r = 2.32. For D = 480, equation (5) provides a curve similar to those shown in FIG. 2, which yields a reflection height H = 330 km for r = 2.32.
The doppler undulation attributed to the one-hop transmission has a half-period T/2 = 24 min. The phase-path behavior is determined by time-integrating the doppler shift. Assuming, however, a sinusoidal undulation of the doppler shift for the event observed on the 7.335 MHz carrier, the corresponding phase-path perturbation amplitude ΔPo (km) can be computed from the period, T(min) and the doppler shift maximum δfo (Hz) by ΔPo = 0.39 δfo T = = 11 km for an undulation period T = 48 min.
Evaluating dP/dH from equation (4) for H = 330 km, D = 480 km and n = 1, one can infer the height change ΔHo, associated with the phase-path perturbation amplitude ΔPo = 11 km, as ΔHo = 7 km. Thus, the ionosphere (reflection level) could be viewed as rising in 12 min by ΔHo = 7 km and over a half-period of 24 min by 14 km, whereupon it descends (positive doppler) starting at 1940 EST. In order to corroborate these results and validate the assumed correspondence between the doppler signatures, a selected set of ionograms, recorded on Mar. 1, 1969 near 1916, 1930, 1940 EST by the Highgate Springs Ionosonde of the Dartmouth College Ionosone network, located 100 km north of the midpoint between CHU and AFCRL, were examined. A transmission curve for 7.335 MHz was superimposed on the ionogram trace obtained for 1930 EST, yielding an equivalent vertical frequency of 5.9 MHz and a virtual reflection-height of 315 km. It was noted, however, that the undulation in reflection height, deduced from the sounder data, preceded by about 5 min those inferred from the doppler data. This suggested that the undulation phenomenon was associated with a wave motion in the ionosphere that raised the height of the F-region over Highgate Springs about 5 min earlier than over the CHU-AFCRL midpoint. Adjusting the reflection height by a translation in space to account for the delay corresponding to about 5 min in time, yielded a reduction from 315 km to 305 km reflection height, as deduced from the ionograms. This result of H = 305 km compares reasonably well with H = 330 km deduced from the multi-hop doppler signatures (see FIG. 3) using the ratio-method based on the simple geometry of FIG. 1.
Another corroborating evidence can be inferred from the height excursions associated with wave phenomenon as deduced from the ionograms, yielding ΔHI = ± 13 km, and those from the doppler variation, yielding ΔHD = ± 7 km. The ratio of these quantities is nearly two, as previously noted for a nighttime wave disturbance in the ionosphere.
In regard to errors of r affecting the percent of errors of height determination, there was assembled a table with data taken from curve "D = 500 km" of FIG. 2. Errors in percent are derived from geometrical considerations only. For D = 500 km, the smallest error obtains for a height of 150 km. For D = 1000 km, the smallest error would result at H = 220 km. Thus, the optimal accuracy of the ratio method for a particular height regime of interest is achieved for a particular distance D. Departure from optimal accuracy is faster toward lower heights than toward greater heights. For D = 500 km the accuracies achievable for heights above the E region may be satisfactory for most of the ratio errors.
For a severely disturbed ionosphere, the presence of small-scale irregularities could preclude the identification of one- and two-hop transmissions because of signal scatter and increased attenuation. Under those conditions, and for lack of signal quality, it may not be possible to successfully apply the ratio method for obtaining height information.
The general limitation of the sensitive doppler method being useful only for determining relative phase-path variations of ionospherically reflected radio signals, has been extended by the finding that the ratios of multi- and single-hop doppler shifts could yield useful information on ionospheric reflection height.

Claims (3)

What is claimed is:
1. The method for determining the ionospheric reflection height from doppler measurements over an oblique CW radio transmission being comprised of transmitting from a first predetermined position first and second identical CW signals obliquely toward a radial moving ionospheric boundary, said first and second signals being single-hop and multi-hop, respectively, receiving at a second predetermined position displaced from said first predetermined position said first and second signals, the radial motion of said boundary imparting different rate-of-phase-path changes to the one-hop, multi-hop transmissions causing a separate doppler shift for each at the receiver and determining said ionospheric boundary height from the doppler ratio of each of said received one-hop and multi-hop transmissions.
2. The method for determining the ionospheric reflection height as described in claim 1 wherein the doppler ratio is comprised of (dP/dH)n =2 / (dP/dH)n =1 where H equals height and P the total path between transmitting position, reflection boundary and receiving position.
3. The method for determining the ionospheric reflection as described in claim 2 further including computing the ionospheric height from the doppler ratio.
US05/678,321 1976-04-19 1976-04-19 Method of determining ionospheric reflection height Expired - Lifetime US4011565A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US05/678,321 US4011565A (en) 1976-04-19 1976-04-19 Method of determining ionospheric reflection height

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/678,321 US4011565A (en) 1976-04-19 1976-04-19 Method of determining ionospheric reflection height

Publications (1)

Publication Number Publication Date
US4011565A true US4011565A (en) 1977-03-08

Family

ID=24722323

Family Applications (1)

Application Number Title Priority Date Filing Date
US05/678,321 Expired - Lifetime US4011565A (en) 1976-04-19 1976-04-19 Method of determining ionospheric reflection height

Country Status (1)

Country Link
US (1) US4011565A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5428358A (en) * 1994-05-03 1995-06-27 The United States Of America As Represented By The Secretary Of The Navy Apparatus and method for ionospheric mapping
US20030156056A1 (en) * 2000-07-26 2003-08-21 Perry Kenneth H Near-vertical incidence hf radar
US7307577B1 (en) * 2006-09-28 2007-12-11 Rockwell Collins, Inc. Storm top detection
CN101813762A (en) * 2010-04-23 2010-08-25 中国航空无线电电子研究所 Airborne single baseline Doppler-phase difference direction finding method
US20100245163A1 (en) * 2009-03-24 2010-09-30 U.S.A. As Represented By The Administrator Of The National Aeronautics And Space Administration Step frequency isar
CN102004244A (en) * 2010-08-12 2011-04-06 中国航空无线电电子研究所 Doppler direct distance measurement method
US8742974B1 (en) 2011-09-27 2014-06-03 Rockwell Collins, Inc. System and method for enabling display of textual weather information on an aviation display
US8786486B1 (en) 2011-09-27 2014-07-22 Rockwell Collins, Inc. System and method for providing weather radar status
US9411044B1 (en) 2011-09-27 2016-08-09 Rockwell Collins, Inc. Auto updating of weather cell displays
US9941950B2 (en) 2014-12-11 2018-04-10 Skywave Networks Llc Communication method and system that uses low latency/low data bandwidth and high latency/high data bandwidth pathways
US11496210B2 (en) 2017-10-04 2022-11-08 Skywave Networks Llc Adjusting transmissions based on direct sensing of the ionosphere

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3333264A (en) * 1964-05-22 1967-07-25 Dornier System Gmbh Method and apparatus for determining the accuracy of projectiles fired at a target
US3665466A (en) * 1970-03-20 1972-05-23 Exxon Production Research Co Determination of ice thickness

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3333264A (en) * 1964-05-22 1967-07-25 Dornier System Gmbh Method and apparatus for determining the accuracy of projectiles fired at a target
US3665466A (en) * 1970-03-20 1972-05-23 Exxon Production Research Co Determination of ice thickness

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5428358A (en) * 1994-05-03 1995-06-27 The United States Of America As Represented By The Secretary Of The Navy Apparatus and method for ionospheric mapping
US20030156056A1 (en) * 2000-07-26 2003-08-21 Perry Kenneth H Near-vertical incidence hf radar
US6831592B2 (en) * 2000-07-26 2004-12-14 Alenia Marconi Systems Limited Near-vertical incidence HF radar
US7307577B1 (en) * 2006-09-28 2007-12-11 Rockwell Collins, Inc. Storm top detection
US8138961B2 (en) * 2009-03-24 2012-03-20 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Step frequency ISAR
US20100245163A1 (en) * 2009-03-24 2010-09-30 U.S.A. As Represented By The Administrator Of The National Aeronautics And Space Administration Step frequency isar
CN101813762B (en) * 2010-04-23 2012-05-23 中国航空无线电电子研究所 Airborne single baseline Doppler-phase difference direction finding method
CN101813762A (en) * 2010-04-23 2010-08-25 中国航空无线电电子研究所 Airborne single baseline Doppler-phase difference direction finding method
CN102004244A (en) * 2010-08-12 2011-04-06 中国航空无线电电子研究所 Doppler direct distance measurement method
CN102004244B (en) * 2010-08-12 2012-10-03 中国航空无线电电子研究所 Doppler direct distance measurement method
US8742974B1 (en) 2011-09-27 2014-06-03 Rockwell Collins, Inc. System and method for enabling display of textual weather information on an aviation display
US8786486B1 (en) 2011-09-27 2014-07-22 Rockwell Collins, Inc. System and method for providing weather radar status
US9411044B1 (en) 2011-09-27 2016-08-09 Rockwell Collins, Inc. Auto updating of weather cell displays
US9941950B2 (en) 2014-12-11 2018-04-10 Skywave Networks Llc Communication method and system that uses low latency/low data bandwidth and high latency/high data bandwidth pathways
US10778323B2 (en) 2014-12-11 2020-09-15 Skywave Networks Llc Communication method and system that uses low latency/low data bandwidth and high latency/high data bandwidth pathways
US11581940B2 (en) 2014-12-11 2023-02-14 Skywave Networks Llc Communication method and system that uses low latency/low data bandwidth and high latency/high data bandwidth pathways
US11496210B2 (en) 2017-10-04 2022-11-08 Skywave Networks Llc Adjusting transmissions based on direct sensing of the ionosphere
US12068837B2 (en) 2017-10-04 2024-08-20 Skywave Networks Llc Adjusting transmissions based on direct sensing of the ionosphere

Similar Documents

Publication Publication Date Title
US2301929A (en) Radio distance and altitude indicating system
US6529165B1 (en) Radio positioning systems
US2408048A (en) Radio direction method and system
Chestnut Emitter location accuracy using TDOA and differential Doppler
US4011565A (en) Method of determining ionospheric reflection height
US5173690A (en) Passive ranging system utilizing range tone signals
Ahmad et al. Doppler effect in the acoustic ultra low frequency band for wireless underwater networks
Austin The application of spread spectrum signaling techniques to underwater acoustic navigation
CN106483495A (en) A kind of indoor sport tag location and speed-measuring method
US5684489A (en) Position-finding apparatus for locating a vehicle travelling along means for propagating electromagnetic waves
US4350984A (en) Method of position fixing active sources utilizing differential doppler
KR0122764B1 (en) Transducer device for acoustic log
US2467455A (en) Radio speed and distance indicator
JP4893883B2 (en) Radio altitude speed measuring apparatus and altitude speed measuring method using radio wave
Wang et al. Water velocity and level monitoring based on UAV radar
US5760733A (en) Apparatus for avoiding crosstalk problems when locating a vehicle travelling along means for propagating electromagnetic waves
US2742638A (en) Radio ranging system
US4564841A (en) Navigational systems using phase encoded angular coordinates
US2986732A (en) Navigation system
US3594790A (en) Position location system and method
US3242490A (en) Apparatus for and a method of determining the position of electromagnetic noise source
RU2380723C1 (en) Method for detection of radiation source motion parameters
NO139938B (en) PROCEDURE FOR DETERMINING THE MOVEMENT OF MOVEMENT THROUGH BY A VESSEL
Gossard et al. Movement of off-path ionospheric irregularities deduced from short-path VLF measurements
US3274599A (en) Radio direction finder system